View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 19257U 26018.66939750 +.00000000 +00000-0 +32545-4 0 00002
2 19257 74.0454 204.6564 0019494 35.3226 35.1331 14.38880840 05
| Epoch (UTC): | 18 January 2026 16:03:55 |
| Eccentricity: | 0.0019494 |
| inclination: | 74.0454° |
| perigee height: | 748 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 204.6564° |
| argument of perigee: | 35.3226° |
| revolutions per day: | 14.38880840 |
| mean anomaly at epoch: | 35.1331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|